N16894
Registered owner: SAZ DYNAMICS LLC, CA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| U.S. Marshals Service, Dept. of Justice | Operator | on 2004-09-26 | Operator named in NTSB report |
Accident & incident history
Operated by U.S. Marshals Service, Dept. of Justice (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
47 reports on file, 1995-01-08 – 2002-04-19.
Part: BULKHEAD — CORRODED (FS 120) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND BULKHEAD CORRODED FORWARD OF FIRST OFFICER'S I/B SEAT TRACK AT FS 120, LBL 30 TO RBL 58. THE BULKHEAD WAS REPAIRED IAW SRM 53-01, FIGURE 2.
Part: SKIN — GOUGED (FS 1510) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND FUSELAGE SKIN GOUGED UNDER R/H RAIN GUTTER AT FS 1510. THE GUTTER WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-20-1.
Part: FLOOR PANEL — SPLIT (FS 218-256) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND CHANNEL ON BACK OF MAIN CABIN DECK FLOOR PANEL AT FS 218-256, RBL 44-58, COMING LOOSE AND PANEL WAS SPLITTING AT THE END. THE PANEL AND CHANNEL WERE REPAIRED IAW SRM 51-70-2 AND 51-20-1.
Part: WIRE — DISCONNECTED (EMER LT CONN) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT 14R AND 15R. TROUBLESHOOTING FOUND CONNECTOR AT 15R HAD A PUSHED PIN. THE PIN WAS RESEATED IAW MM 20-50-01. SEAT 14R HAD GROUND WIRE PULLED FROM CONNECTOR SPLICE. THE GROUND WIRE AT CONNECTOR WAS RESEATED IAW MM 20-50-01. OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00.
Part: SHEAR TIE — CRACKED (STA 1307) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND A 1" CRACK IN SKIN TO FRAME SHEAR TIE AT STA 1307, LONGERON 15R LAV BULKHEAD. THE #2 ENGINE WAS REMOVED FOR ACCESS. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-04 AND 51-30-5. THE #2 ENGINE WAS REINSTALLED.
Part: WIRE — BROKEN (L2 DOOR) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND L-2 DOOR EXIT LIGHT INOPERATIVE. CHECKED WIRING AT AFT DROP CEILING AND FOUND POWER WIRE BROKEN AT WIRE CONDUIT. THE POWER WIRE WAS RESPLICED. NO GROUND WIRE WAS FOUND GOING TO SIGN. CONNECTED GROUND WIRE AND OPERATIONAL CHECKS WERE GOOD IAW WDM 33-51-14.
Part: INTERCOSTAL — CORRODED (FS 769-786) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO AREA BETWEEN FS 769 AND 786, L27L-L28L. THE INTERCOSTAL WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
Part: SKIN — DENTED (VENTRAL STAIR) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND VENTRAL STAIRS EXTERNAL SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-01, FIGURE 1 AND 51-10-3.
Part: FITTING — CORRODED (STA 200-216) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND GALLEY FITTING CORRODED AT STA 200-216, RBL 22, UPON REMOVAL OF SUBFLOOR WEB. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.
Part: SKIN — CRACKED (R/H MLG DR) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND A 1/2" CRACK IN THE R/H MLG I/B DOOR SKIN AT LOWER FORWARD EDGE. THE DOOR SKIN WAS REPAIRED IAW EA 9-5281-2-A0941 AND ECRA 5281-01020.
Part: WEB — CORRODED (FUSELAGE) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND FLOOR WEB CORRODED AT FS 120-133, LBL 28 TO RBL 84. THE O/B PILOT SEAT TRACK WAS REMOVED IAW SRM 51-30-1. THE FLOOR SUPPORT AND WEB WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.
Part: SEAT TRACK — CORRODED (STA 110-120) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND COCKPIT SEAT TRACK CORRODED AT STA 110-120, RBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01.
Part: SEAT TRACK — CORRODED (STA 110-120) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND SEAT TRACK CORRODED AT STA 110-120, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0.
Part: SKIN — DENTED (FLAP VANE) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND R/H I/B FLAP O/B VANE LOWER SKIN SURFACE DENTED. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-1.
Part: SEAT TRACK — CORRODED (STA 120-148) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND CAPTAIN'S I/B SEAT TRACK CORRODED AT STA 120-148, LBL 15. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5.
Part: ANGLE — CORRODED (L-2 DR JAMB) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND L-2 DOOR LOWER FORWARD DOOR JAMB L-ANGLE CORRODED AT STA 1138, 18L. THE SCUFF PLATE WAS REMOVED TO GAIN ACCESS IAW SRM 51-30-1. THE L-2 DOOR WAS REMOVED IAW MM 52-42-00. THE ANGLE AND FITTING WERE REMOVED AND A NEW ANGLE AND SPLICE WAS INSTALLED IAW EA 9-5310-2-A0945. INSTALLED SCUFF PLATE IAW SRM 51-30-1. THE L-2 DOOR WAS INSTALLED AND RIGGED IAW MM 52-42-00.
Part: SEAT TRACK — CORRODED (CO-PILOT SEAT) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND L/H AND R/H FORWARD UPPER CO-PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92.
Part: FLOORBEAM — CORRODED (STA 120) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND UPPER CAP(ANGLE) OF FLOORBEAM CORRODED IN E&E COMPARTMENT OVERHEAD AT STA 120, RBL 15 TO RBL 30. THE ANGLE WAS REMOVED AND A NEW ANGLE AND REPAIR SPLICES WERE INSTALLED IAW SRM 51-10-4.
Part: SEAT TRACK — CORRODED (PILOT SEAT) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND R/H AND L/H FORWARD UPPER PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92.
Part: SUPPORT — CRACKED (STA 1485-1497) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND A 2" CRACK IN SUPPORT IN AFT ACCESSORY COMPARTMENT BETWEEN CANTED FRAMES STA 1485 AND 1497 AND BELOW LEFT AIRSTAIR TORQUE TUBE. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, AND 51-10-3.
Part: FITTING — CORRODED (STA 155) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 155, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-2.
Part: SKIN — CRACKED (FWD CARGO DR) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND FORWARD EDGE OF FORWARD CARGO DOOR SKIN CRACKED AND BENT JUST ABOVE LOCK MECHANISM AND SEAL. THE CRACK MEASURED 0.4" LONG. THE EXISTING FASTENERS WERE REMOVED, THE CRACK WAS STOP DRILLED, AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 52-05, FIGURE 4.
Part: SKIN — DENTED (#1 FLAP VANE) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND L/H WING #1 I/B FLAP VANE DENTED AND PUNCTURED. THE DAMAGED AREA OF SKIN WAS CUT OUT. FILLERS AND A DOUBLER WERE INSTALLED IAW SRM 57-03 AND 51-70-2.
Part: SEAT TRACK — CORRODED (STA 1098-1174) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND L/H I/B SEAT TRACK CORRODED FROM STA 1098-1174. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, 51-30-5, AND 53-05, FIGURE 4.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND 1 INCH CRACKS AT FLOOR PANEL INSERTS, FS 1003. THE FLOOR PANEL WAS REPAIRED.
Part: SKIN — GOUGED (R/W T/E FLAP) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND R/H WING I/B T/E FLAP PANEL #1613C SKIN NICKED AND GOUGED. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-3.
Part: LONGERON — CRACKED (FS 1003) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND A 1.75" CRACK AT LOWER RADIUS OF LONGERON 20R EXTERNAL FITTING, FS 1003. THE CRACKED AREA WAS REMOVED IAW EA 9-5310-2-A0942 AND HFEC REVEALED NO FURTHER CRACKS IAW NTSPM 06-10-01. REPAIR PARTS WERE INSTALLED IAW EA 9-5310--2-A0942.
Part: SEAT TRACK — CORRODED (STA 237) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT STA 237, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND FLOOR PANEL CORRODED AT STA 180, LBL 10 - RBL 55. THE CORRODED DOUBLER WAS REMOVED FROM THE WEB AND A REPAIR DOUBLER WAS INSTALLED.
Part: SUPPORT — CORRODED (STA 541) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND FORWARD BULKHEAD LOWER CENTER SUPPORT FRAME HAD CLIP-NUTS AND ATTACH HOLES CORRODED IN MID CARGO COMPARTMENT AT STA 541. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
Part: INTERCOSTAL — CORRODED (FS 769-786) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO COMPARTMENT AT FS 769-786 BETWEEN L27R AND 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: PAN — CORRODED (STA 370-420) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND PAN CORRODED AT FORWARD CARGO DOOR CUTOUT AREA, STA 370-420. THE CORROSION WAS BETWEEN SCUFF PLATE AND JAMB. THE PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44.
Part: SEAT TRACK — CORRODED (STA 1146) · airframe 49,164 hrs · 24,367 cycles
INSPECTION FOUND SEAT TRACK CORRODED AT STA 1146, LBL 40. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-10-3.
Earlier reports · 1995–2001 · 14 reports
2001
Part: WIRE ROPE — FRAYED (TAILCONE) · airframe 46,853 hrs · 23,143 cycles
THE TAIL CONE DID NOT RELEASE WHEN PULLED FROM AFT ENTRANCE DOOR. THE TAIL CONE CABLE WAS FOUND FRAYED. THE CABLE WAS REPLACED AND A TAIL CONE ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 46,853 hrs · 23,143 cycles
INSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER FLANGE OF RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463 JUST FORWARD OF VERTICAL STABILIZER REAR SPAR PLANE. A REPAIR DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 46,853 hrs · 23,143 cycles
MID BAG BIN DOOR JAMB Z CHANNEL HAS CORROSION AROUND HI-SHEARS. INSTALLED DOUBLER AND SPACER PER SRM 53-05 FIG 63.
Part: STRUT — INOPERATIVE (NLG) · airframe 46,020 hrs · 22,690 cycles
THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED ACCOMPANIED BY NOISE AND BUFFETING AFTER TAKEOFF FROM ATL. THE AIRCRAFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NLG STRUT WAS REPACKED IAW MM 32-21-02. LEAK CHECKS WERE GOOD. A NOSE GEAR RETRACTION WAS PERFORMED IAW MM 32-20-00, PAGE 201 AND NO FAULTS WERE NOTED.
1999
Part: SKIN — CRACKED (PAX DOOR)
INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR SKIN AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-05, FIGURE 32.
Part: BELTFRAME — CORRODED (BS 1322)
HEAVY CORROSION ON LOWER FORWARD FLANGE AND FWD FACE OF BELT FRAME AT STA 1322 L28 TO R28. REPAIRED PER SRM 53-03.
Part: SKIN — CORRODED (BS 198)
FWD WATER DRAIN MAST MOUNT STRUCTURE HAS CORROSION INSIDE E & E COMPARTMENT STA 198 RIGHT OF CENTER. REMOVED AND REPLACED INTERCOSTAL, DOUBLER AND DRAIN MAST PER SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 1136 - 1155)
CORROSION ON LEFT INBOARD SEAT TRACK STA 1136 TO 1155. REPAIRED PER SRM 53-05.
Part: BEAM — CRACKED (SERVICE DOOR)
FORWARD SERVICE DOOR HORIZONTAL BEAM HAS 4 CRACKS IN RADIUS WHERE LOWER HINGE ATTACHES. REPLACED HORIZONTAL BEAM PER SRM 51-30-2.
Part: SKIN — DENTED (BS 218-225)
FORWARD FUSELAGE SKIN SCRATCHED AND DENTED STA 218 TO 225 BETWEEN LONG 15L AND 18L. REPAIRED PER EC/RA 5330-02445.
1998
Part: HYD LINE — LEAKED (CARGO COMPT)
SMOKE APPEARED IN THE CABIN AFTER TAKEOFF AND BEGAN CLEARING WITHIN 2-3 MINUTES. THE SMOKE HAD COMPLETELY DISSIPATED WITHIN 10-15 MINUTES. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE IN THE AFT CARGO COMPARTMENT LEAKING CAUSING HYDRAULIC FLUID TO BE INGESTED BY APU. THE LINE WAS REPAIRED IAW GENERAL MAINTENANCE MANUAL 10-799-78. AN ENGINE RUN WAS PERFORMED WITH PACKS OPERATING AND NO SMOKE WAS NOTED.
Part: RETRACT MECH — MALFUNCTIONED (NLG)
THE NLG DID NOT RETRACT AFTER TAKEOFF. BOTH THE RED NOSE GEAR LIGHT AND YELLOW GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FAULT WAS ACCOMPANIED BY LOUD WIND NOISE AND VIBRATION. THE GEAR WAS CYCLED AND THE NOSE GEAR RETRACTED WITH GOOD INDICATIONS. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SEVERAL TIMES WITH NO FAULTS NOTED. THE NLG STRUT WAS SERVICED IAW MM 32-21-02.
1996
Part: SKIN — CRACKED (AFT SERVICE DOOR)
INSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN ABOVE AND BELOW HOLD OPEN HOOK. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01340 AND SRM 52-01.
1995
Part: LATCHES — LACK OF LUBE (TAIL CONE)
HOU - THE TAIL CONE INTERIOR RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE LATCHES WERE LUBRICATED AND THE INTERIOR RELEASE HANDLE PULL FORCE CHECKED GOOD PER MM 53-50-00. (X)